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AMP · 7% of the exam

Engine Instrument Systems practice questions

10 free Engine Instrument Systems questions for the Aviation Mechanic Powerplant (AMP) Knowledge Test exam, each with the correct answer and an explanation for every option.

What this domain covers

Engine instruments: what they measure and how they work.

Exam weight
7%
On a real exam
≈ 7 questions
In our bank
43 questions

Topics that come up most

  • Temperature indicators
  • Pressure indicators
  • Tachometers
  • Fuel-flow and quantity indication
  • Instrument markings

How to study it

Know the instrument range markings and what each colour means.

Sample Engine Instrument Systems questions

Try each one before opening the answer. Original questions written to the official exam objectives.

  1. Question 1

    Which mechanism is used in a direct-reading oil pressure gauge?

    • AA thermocouple
    • BA Bourdon tube
    • CA synchro motor
    • DA float arm
    Show answer and explanation

    Answer: B) A Bourdon tube

    • AIncorrect. This measures temperature.
    • BCorrect. Pressure straightens the curved Bourdon tube, moving the pointer.
    • CIncorrect. This is a remote indication method.
    • DIncorrect. This measures level.
  2. Question 2

    Turbine engine EGT is usually indicated in:

    • APounds per hour
    • BDegrees Celsius
    • CPercent RPM
    • DInches of mercury
    Show answer and explanation

    Answer: B) Degrees Celsius

    • AIncorrect. That's fuel flow.
    • BCorrect. Limits are published in °C.
    • CIncorrect. That's N1 or N2.
    • DIncorrect. That's manifold pressure.
  3. Question 3

    On a turbofan, the N1 indication shows:

    • AFuel temperature
    • BOil tank level
    • CCore spool speed
    • DFan spool speed
    Show answer and explanation

    Answer: D) Fan spool speed

    • AIncorrect. This is not N1.
    • BIncorrect. This is a quantity reading.
    • CIncorrect. That is N2.
    • DCorrect. N1 is low-pressure spool (fan) speed, often a thrust-setting parameter.
  4. Question 4

    During a ground run-up, a multi-probe EGT system shows five cylinders reading close together while one cylinder reads far below the rest. Which condition is the most likely cause?

    • AThat cylinder is misfiring or not firing, such as from a fouled plug or faulty ignition lead
    • BThe mixture control is set too rich for the current power setting
    • CThe ignition timing on both magnetos is retarded from the specified setting
    • DThe engine oil cooler is partially blocked, restricting oil flow
    Show answer and explanation

    Answer: A) That cylinder is misfiring or not firing, such as from a fouled plug or faulty ignition lead

    When one cylinder's EGT is far below otherwise matching cylinders, that cylinder is probably not burning its charge, for example because of a fouled plug, a bad lead or a fuel delivery problem. Mixture or timing faults affect all cylinders together.

    • ACorrect. If a cylinder burns little or no fuel/air charge, little heat reaches its exhaust, so its EGT probe reads well below the others. Check that cylinder's plugs, ignition leads and fuel delivery.
    • BIncorrect. A rich mixture setting lowers EGT on every cylinder fed by the mixture control, not on just one while the others stay close together.
    • CIncorrect. Retarded timing affects every cylinder and tends to raise EGT, because combustion is still going on as the exhaust valve opens. It would not single out one cylinder with a low reading.
    • DIncorrect. A restricted oil cooler shows up as high oil temperature. It does not make one cylinder's exhaust gas temperature drop.
  5. Question 5

    When instrument range markings are painted on the cover glass, a slippage mark is required to:

    • AShow the fuel type
    • BIndicate maximum RPM
    • CMark the caution operating range
    • DShow if the glass has rotated
    Show answer and explanation

    Answer: D) Show if the glass has rotated

    • AIncorrect. That isn't its purpose.
    • BIncorrect. That's the red line.
    • CIncorrect. That's the yellow arc.
    • DCorrect. A white index line reveals movement.
  6. Question 6

    A restrictor in a direct-reading oil pressure gauge line mainly:

    • AHeats the oil so the gauge reads accurately
    • BRaises oil pressure in the engine
    • CDampens pulsations and limits leakage
    • DMeasures oil temperature
    Show answer and explanation

    Answer: C) Dampens pulsations and limits leakage

    • AIncorrect. That isn't its role.
    • BIncorrect. It doesn't change engine pressure.
    • CCorrect. It also limits oil loss if the line breaks.
    • DIncorrect. That's a temperature probe.
  7. Question 7

    Turbine engine fuel flow is usually indicated in:

    • ADegrees Celsius
    • BInches of mercury
    • CPounds per hour
    • DPercent RPM
    Show answer and explanation

    Answer: C) Pounds per hour

    • AIncorrect. That is a temperature unit.
    • BIncorrect. That is a pressure unit.
    • CCorrect. Mass flow in pounds per hour reflects energy delivered.
    • DIncorrect. That is a speed indication.
  8. Question 8

    On a gas turbine engine, where is the temperature probe for interstage turbine temperature (ITT) located?

    • AAt the inlet to the first-stage turbine nozzle guide vanes
    • BBetween the high-pressure (gas generator) turbine and the low-pressure turbine
    • CIn the exhaust duct downstream of the last turbine stage
    • DAt the compressor diffuser outlet ahead of the combustors
    Show answer and explanation

    Answer: B) Between the high-pressure (gas generator) turbine and the low-pressure turbine

    ITT is sensed between the high-pressure and low-pressure turbines; on free-turbine engines, that is between the compressor turbine and the power turbine. TIT is measured ahead of the first turbine stage, and EGT is measured after the last one.

    • AIncorrect. Gas temperature entering the first-stage turbine inlet guide vanes is turbine inlet temperature (TIT), not ITT.
    • BCorrect. ITT is the gas temperature between the high-pressure turbine and the low-pressure turbine. On a free-turbine engine, that is between the compressor (gas generator) turbine and the power turbine.
    • CIncorrect. A probe after the last turbine stage measures exhaust gas temperature (EGT), also called turbine outlet temperature, not interstage temperature.
    • DIncorrect. This location gives compressor discharge temperature, which is upstream of combustion and of the turbines.
  9. Question 9

    Many digital tachometers sense engine speed with:

    • AA magnetic pickup
    • BA Bourdon tube
    • CA thermocouple
    • DA float
    Show answer and explanation

    Answer: A) A magnetic pickup

    • ACorrect. Gear teeth passing it produce pulses.
    • BIncorrect. That measures pressure.
    • CIncorrect. That measures temperature.
    • DIncorrect. That measures level.
  10. Question 10

    On transport aircraft equipped with EICAS, the system's display units take over the job of which conventional cockpit equipment?

    • AWeather radar indicator and the terrain awareness display
    • BIndividual engine gauges and separate warning and caution lights
    • CPrimary flight display attitude and airspeed presentations
    • DFlight management computer route and navigation database pages
    Show answer and explanation

    Answer: B) Individual engine gauges and separate warning and caution lights

    EICAS combines engine parameter indications and crew alerting (warning, caution and advisory messages) on electronic displays. It replaces the separate engine gauges and annunciator lights of older cockpits.

    • AIncorrect. Weather radar and terrain information usually appear on the navigation display (EFIS), not on the EICAS engine and alerting displays.
    • BCorrect. EICAS (engine indicating and crew alerting system) shows primary and secondary engine parameters on electronic display units, along with warning, caution and advisory messages. This replaces the many separate engine gauges and annunciator lights found in older cockpits.
    • CIncorrect. Attitude and airspeed are shown on the primary flight display, which is part of the EFIS, not on EICAS.
    • DIncorrect. Route and navigation database information is handled by the flight management system and its control display unit, not by EICAS.

Engine Instrument Systems: FAQs

How much of the AMP exam is Engine Instrument Systems?

Engine Instrument Systems is 7% of the AMP exam by the official exam guide's weighting, which on a 100-question form works out to roughly 7 questions. The real exam's exact split varies by form.

What does the Engine Instrument Systems domain cover?

Engine instruments: what they measure and how they work.

How should I study Engine Instrument Systems for AMP?

Know the instrument range markings and what each colour means.

Where can I practise more Engine Instrument Systems questions?

This page has 10 free Engine Instrument Systems questions with answers. The ExamWize AMP question bank has 43 questions in this domain. Every practice exam result breaks your score down by domain, and Review Mode re-drills the questions you missed.

Get Engine Instrument Systems exam-ready

The full AMP bank has 43 Engine Instrument Systems questions. Timed practice exams match the real exam's length and domain weights, every result shows your score per domain, and Review Mode re-drills the questions you missed.

Not affiliated with FAA; questions are original, written from the official exam outline, and never copied from the real exam.